Payload support frame for unmanned aerial system
An apparatus, system, and/or method for carrying a power line device from an aircraft, such as an unmanned aerial vehicle (UAV), and for performing work on electrical power lines and/or splices on electrical power lines. The apparatus or system may include an attachment flange selectively and releasably coupled to the aircraft, a payload support frame selectively and releasably coupled to the attachment flange, an intermediary frame selectively and releasably coupled to the payload support frame, and a base frame selectively and releasably coupled to the power line device. The payload support frame may include at least three elongated rigid segments, each including a hollow elongated pole, at least three upper flexible segments, each at an upper end of a corresponding rigid segment, and at least three lower flexible segments, each at a lower end of a corresponding rigid segment.
1. An apparatus comprising:
an attachment flange selectively and releasably coupled to an unmanned aerial vehicle (UAV);
a payload support frame selectively and releasably coupled to the attachment flange, wherein the payload support frame comprises:
at least three elongated rigid segments, each elongated rigid segment comprising a hollow elongated pole;
at least three upper flexible segments, each upper flexible segment positioned at an upper end of a corresponding rigid segment; and
at least three lower flexible segments, each lower flexible segment positioned at a lower end of a corresponding rigid segment;
an intermediary frame selectively and releasably coupled to the payload support frame via the at least three lower flexible segments, wherein the intermediary frame is coupled to a power line device at one or more points, wherein the power line device is configured to measure one or more properties of an electrical power line and/or a splice on the electrical power line; and
a base frame selectively and releasably coupled to the power line device.
2. The apparatus of claim 1 , wherein each upper flexible segment of the at least three upper flexible segments and each corresponding lower flexible segment of the at least three lower flexible segments comprise a single rope, cable, or wire and are coupled to a corresponding one of the elongated poles.
3. The apparatus of claim 1 , wherein each of the elongated poles comprise one or more interconnecting pole segments.
4. The apparatus of claim 3 , wherein a length of each elongated pole is adjusted based on removing, replacing, or adding one or more of the interconnecting pole segments.
5. The apparatus of claim 1 , wherein a length of each elongated pole is configured to be adjusted based on an electromagnetic field of an energized electrical power line.
6. The apparatus of claim 1 , wherein the base frame comprises at least two guide bars.
7. The apparatus of claim 6 , wherein the guide bars each comprise of one or more segments, wherein at least a portion of each segment is hollow.
8. The apparatus of claim 7 , wherein each of the one or more segments comprise a nonferrous weighted material inside the hollow portion.
9. The apparatus of claim 6 , wherein the guide bars are selectively and releasably coupled to the power line device via cotter pins.
10. The apparatus of claim 1 , wherein the attachment flange comprises at least three attachment points, and wherein the at least three upper flexible segments each comprise an attachment component configured to selectively and releasably connect to one of the at least three attachment points of the attachment flange.
11. The apparatus of claim 1 , further comprising:
a rigid upper spacer frame configured to hold the at least three upper flexible segments, and thereby the upper ends of the corresponding rigid segments, in a spaced-apart arrangement; and
a rigid lower spacer frame configured to hold the at least three lower flexible segments, and thereby the lower ends of the corresponding rigid segments, in a spaced-apart arrangement.
12. The apparatus of claim 11 , wherein the at least three upper flexible segments comprise at least three first upper flexible segments;
wherein the at least three lower flexible segments comprise at least three first lower flexible segments; and
wherein the apparatus further comprises:
at least three second upper flexible segments, each of the at least three second upper flexible segments on an opposite side of the upper spacer frame from a corresponding one of the at least three first upper flexible segments; and
at least three second lower flexible segments, each of the at least three second lower flexible segments on an opposite side of the lower spacer frame from a corresponding one of the at least three first lower flexible segments;
wherein each of the at least three second upper flexible segments and a corresponding one of the at least three first upper flexible segments comprise a single rope, cable, or wire extending through a corresponding channel in the rigid upper spacer frame; and
wherein each of the at least three second lower flexible segments and a corresponding one of the at least three first lower flexible segments comprise a single rope, cable, or wire extending through a corresponding channel in the rigid lower spacer frame.
13. The apparatus of claim 1 , wherein the at least three upper flexible segments and the at least three lower flexible segments comprise a dielectric material.
14. A method for contact inspection of electrical power lines and/or splices on energized electrical power lines, the method comprising:
attaching a power line tool to an unmanned aerial vehicle (UAV) to a payload support apparatus via an attachment flange, wherein the power line tool is adapted to perch on an electrical power line and/or a splice on an electrical power line and wherein the payload support apparatus is selectively releasably attached, directly or indirectly, to the UAV;
piloting the UAV to a position adjacent to and at an altitude that is higher than an energized electrical power line and/or a splice on the electrical power line upon which it is desired to perch the power line tool;
reducing the altitude of the UAV to lower the power line tool onto the power line and/or the splice such that the power line tool is perched on the power line and/or the splice; and
obtaining, by an electronic device, measurement data from the power line tool;
wherein the payload support apparatus comprises the attachment flange, a payload support frame coupled to the attachment flange, an intermediary frame coupled to the payload support frame, and a base frame coupled to the power line tool,
wherein the payload support frame comprises: at least three elongated rigid segments, each elongated rigid segment comprising a hollow elongated pole; at least three upper flexible segments, each upper flexible segment positioned at an upper end of a corresponding rigid segment; and at least three lower flexible segments, each lower flexible segment positioned at a lower end of a corresponding rigid segment.
15. The method of claim 14 , wherein each upper flexible segment of the at least three upper flexible segments and each corresponding lower flexible segment of the at least three lower flexible segments comprise a single rope, cable, or wire and are coupled to a corresponding one of the elongated poles.
16. The method of claim 14 , wherein each of the elongated poles comprise one or more interconnecting pole segments.
17. The method of claim 16 , wherein a length of each elongated pole is adjusted based on removing, replacing, or adding one or more of the plurality of interconnecting pole segments, and the length is configured to be adjusted based on an electromagnetic field of an energized electrical power line.
18. The method of claim 14 , further comprising: further reducing the altitude of the UAV to introduce slack into one or more of the at least three upper flexible segments, one or more of the at least three lower flexible segments, or a combination thereof.
19. The method of claim 14 , wherein the base frame comprises at least two guide bars and that each comprise of one or more segments, wherein at least a portion of each segment is hollow and comprises a nonferrous weighted material inside the hollow portion.